JPS6011320A - Method of molding hole in composite material - Google Patents

Method of molding hole in composite material

Info

Publication number
JPS6011320A
JPS6011320A JP58118620A JP11862083A JPS6011320A JP S6011320 A JPS6011320 A JP S6011320A JP 58118620 A JP58118620 A JP 58118620A JP 11862083 A JP11862083 A JP 11862083A JP S6011320 A JPS6011320 A JP S6011320A
Authority
JP
Japan
Prior art keywords
composite material
holes
molding
resin
fastener
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
JP58118620A
Other languages
Japanese (ja)
Inventor
Yoshiaki Sakatani
酒谷 芳秋
Tetsuya Yamamoto
哲也 山本
Shigeru Nishiyama
茂 西山
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Mitsubishi Heavy Industries Ltd
Original Assignee
Mitsubishi Heavy Industries Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Mitsubishi Heavy Industries Ltd filed Critical Mitsubishi Heavy Industries Ltd
Priority to JP58118620A priority Critical patent/JPS6011320A/en
Publication of JPS6011320A publication Critical patent/JPS6011320A/en
Pending legal-status Critical Current

Links

Abstract

PURPOSE:To form fastener holes at low cost with high quality, by carrying out at the same time the fitting of pins into a composite material by a compression force and the molding of holes when the composite material of fiber and resin is compression molded. CONSTITUTION:A molding material 5 comprising a prescribed number of layers together with a bleeder cloth 6 for regulating the quantity of resin is previously sandwiched between templates 2 that have guide holes at required positions, and after pins 1 are inserted in the guide holes, they are set to a base plate 4 by using a dam 3 as a reference. Then after all of them are covered with a vacuum film 7, the compacting of fibers and the regulating of the quantity of resin are carried out simultaneously by heating under vacuum, and the pins are fitted by using the vacuum. Then they are turned and put on a base plate 4, and all of them are covered with a vacuum film 7, and is heated under pressure to obtain a composite material having fastener holes.

Description

【発明の詳細な説明】 本発明は自動成形されるファスナホール、軸受用穴等の
円形穴、及び四角形、六角形等多角形の穴を持つ複合桐
材製品、例えば航空宇宙機器用構造部品、輸送機器、自
動車、一般産業機器、電気電子部品等に適用できる複合
材料、及び炭素繊維/エポキシ、ケブラー繊維/エポキ
シ等特殊需要にある複合材料の他、一般にFRPと称さ
れる繊維強化型複合祠料等のほとんど全ての複合材料の
ボール成形に適用できるボール成形方法に関するもので
ある。
Detailed Description of the Invention The present invention relates to composite paulownia wood products having automatically formed fastener holes, circular holes such as bearing holes, and polygonal holes such as square and hexagonal holes, such as structural parts for aerospace equipment, In addition to composite materials that can be applied to transportation equipment, automobiles, general industrial equipment, electrical and electronic parts, etc., and composite materials for special needs such as carbon fiber/epoxy and Kevlar fiber/epoxy, fiber-reinforced composite shrines commonly referred to as FRP. This invention relates to a ball forming method that can be applied to ball forming almost all composite materials such as materials.

従来腹合材料に対するファスナボール等の準備手法とし
て最も一般的に行なわれているのは、任意形状に成形さ
れた複合材料にドリル、リーマ等の切削工具を用いて所
定の位置に所望寸法のファスナボール等を機械的に加工
する方法であった。
Conventionally, the most common method for preparing fastener balls, etc. for mating materials is to use a cutting tool such as a drill or reamer to place a fastener of a desired size on a composite material formed into an arbitrary shape. This was a method of mechanically processing balls and the like.

しかしこの方法によると、成形と)1スナホール加工の
2工程を要するため、製作工数が増大する欠点があり、
また強化繊維が炭素繊維等の超硬質物である場合は、そ
の硬さのために切削工具自身の切削力の低下が著るしく
、これに係るドリル本数の準備費用、再研磨費用等が増
大する欠点があった。
However, this method requires two steps: molding and one-snare processing, which has the disadvantage of increasing the number of manufacturing steps.
In addition, if the reinforcing fiber is an ultra-hard material such as carbon fiber, the cutting force of the cutting tool itself will be significantly reduced due to its hardness, which will increase the cost of preparing the number of drills and the cost of re-grinding. There was a drawback.

更に航空機部品等ファスナホール内表面に対しても、高
品質を要求される場合は、切削工具での2次加工による
ファスナホール内表面の欠陥、例えば切削熱等による樹
脂焼け、切削応力による眉間剥離等の発生の危険性があ
った。
Furthermore, when high quality is required for the inner surface of fastener holes such as aircraft parts, defects on the inner surface of fastener holes due to secondary processing with cutting tools, such as resin burning due to cutting heat, etc., and peeling between the eyebrows due to cutting stress, etc. There was a risk of such occurrence.

本発明は炭素繊維/エポキシ樹脂等複合材料に対するフ
ァスナ加工を低コストで、かつ高品質に製作することを
目的とするものである。
The object of the present invention is to process a fastener for a composite material such as carbon fiber/epoxy resin at low cost and with high quality.

即ち、本発明は炭素繊維/エポキシ等複合材料に対する
ファスナホール等の加工方法として、成形中の複合材料
の柔軟な状態において、所望のファスナ形状を持つピン
を成形圧力を利用して複合材料中に分りノ入らせ、その
後の硬化によってファスナホールを自動成形することを
特長とし、特に複合材料のファスナボール加工を1工程
で行なうことにより、工数及び治工具面で従来の2工程
に比べ低コスト化できると共に、ピン形状を考慮するこ
とにより、座くり、段イ1穴等も同時成形可能な複合材
料のホール成形方法を提供せんとするものである。
That is, the present invention provides a method for forming fastener holes, etc. in a composite material such as carbon fiber/epoxy, in which a pin having a desired fastener shape is inserted into the composite material using molding pressure while the composite material is in a flexible state. The feature is that the fastener hole is automatically formed by drilling the holes and then curing them.In particular, by processing the fastener balls of composite materials in one step, the cost is lower in terms of man-hours and tools than the conventional two-step process. The present invention aims to provide a hole forming method for a composite material that can simultaneously form a counterbore, a single step hole, etc. by considering the shape of the pin.

以下本発明の実施例を図面について説明すると、第1図
〜第4図は本発明の実施例を示すファスナホール自動成
形の一例を示す。図において成形用治具は、離型処理し
たスチール製ピン1と、ピン1の案内穴を持ち、所定位
置に正確に成形するため、複合桐材又はセラミック製で
、受は側はゴムでも可のテンプレー1−2、アルミ製ダ
ム3及びスチール又はアルミ昭ベースプレート4により
構成されている。
Embodiments of the present invention will be described below with reference to the drawings. FIGS. 1 to 4 show an example of automatic fastener hole forming according to an embodiment of the present invention. In the figure, the molding jig has a mold-released steel pin 1 and a guide hole for the pin 1, and is made of composite paulownia wood or ceramic in order to accurately mold the pin into the specified position, and the receiver can also be made of rubber on the side. It consists of a template 1-2, an aluminum dam 3, and a steel or aluminum base plate 4.

そして第1図は、ベースプレー1〜4上にテンプレート
2によりサンドインチされた成形素材5とピン1をセッ
トした状態を、第2図は繊維の緻密化工程でピンlが真
空圧力により、成形素材5中に分は入って行く様子を、
第3図はピン1が成形素材5を貫通した状態での硬化工
程を示す。また第4図はピン形状を変え、各種ファスナ
ホールを成形し得る状況を示したものである。
Figure 1 shows the state in which the molding material 5 sandwiched by the template 2 and the pin 1 are set on the base plates 1 to 4, and Figure 2 shows the pin 1 being molded by vacuum pressure during the fiber densification process. How the minutes go into material 5,
FIG. 3 shows the hardening process with the pin 1 penetrating the molding material 5. Moreover, FIG. 4 shows a situation in which various fastener holes can be formed by changing the shape of the pin.

本発明は複合材料に対するファスナボール等を成形硬化
工程で同時成形することにより、低二1スト、高品質に
準備せしめる方法に係るものであり、以下にその成形方
法を述べる。
The present invention relates to a method of preparing a fastener ball or the like of a composite material with a low 21st stroke and high quality by simultaneously molding it in a molding and curing process, and the molding method will be described below.

先ず第1図において、予め必要穴位置に案内穴を持った
テンプレート2の間に、所定枚数積層した成形素材5を
樹脂量を調整するためのブリーダクロス6と共にサンド
インチし、案内穴にピン1を挿入後、ベースプレート4
にダム3を基準にセントする。
First, in FIG. 1, a predetermined number of laminated molding materials 5 are sandwiched together with a bleeder cloth 6 for adjusting the amount of resin between templates 2 that have guide holes at required hole positions, and pins 1 are inserted into the guide holes. After inserting the base plate 4
cents based on Dam 3.

次に第2図において、バキュームフィルム7で全体を覆
った後、加熱、減圧することにより繊維の緻密化および
樹脂量の調整を行なうと同時に、柔軟になった樹脂とl
Ji維間に減圧力を利用してピンを分&、J入らせ、本
硬化の準備を完了する。
Next, in Fig. 2, after covering the entire body with a vacuum film 7, the fibers are densified and the amount of resin is adjusted by heating and reducing the pressure.
The pins are inserted between the Ji fibers using reduced pressure to complete the preparation for main curing.

また繊維の緻密化工程を完了した積層体は、次に第3図
の如く反転し、ベースプレート4に置かれて再びバキュ
ームフィルム7で全体を覆った後、加熱、加圧されて本
硬化が行なわれる。本硬化が終了した櫃層体は、全ての
成形治具類が取除かれ、ファスナボール等を持った複合
材料となる。
Further, the laminate which has undergone the fiber densification process is then turned over as shown in Figure 3, placed on the base plate 4, covered again with the vacuum film 7, and then heated and pressurized to perform main curing. It can be done. After the final curing, all molding jigs are removed from the case layer body, which becomes a composite material with fastener balls and the like.

本発明にお゛けるファスナホール等自動成形法を使用す
ることにより、従来2工程で行なって来た成形加工作業
が、■工程となり、成形加工時間の短縮、使用工具の削
減など低コストの製作が可能になると共に、ファスナボ
ールの機械加工によって生ずるファスナボール内表面の
欠陥発生もなくなる等の効果が得られる。
By using the automatic forming method for fastener holes, etc. of the present invention, the forming process, which was conventionally performed in two steps, is reduced to step 1, resulting in low-cost production such as shortening the forming process time and reducing the number of tools used. In addition to this, it is possible to obtain effects such as eliminating defects on the inner surface of the fastener ball caused by machining of the fastener ball.

【図面の簡単な説明】[Brief explanation of the drawing]

第1図、第2図及び第3図は夫々作動状態を異にする本
発明の実施例を示すファスナ自動成形方法を示す断面図
、第4図(イ)(ロ)は夫々ピンの座くり及び段付穴の
場合を示すW1面図である。 図の主要部分の説明 1−・−ピン 2−テンプレート 3−ダム 4−ベースプレー1・ 、 5−成形素材 特許出願人 三菱重工業株式会社 第3図
1, 2 and 3 are sectional views showing an automatic fastener forming method showing embodiments of the present invention in different operating states, and FIGS. and FIG. 1 is a W1 side view showing the case of a stepped hole. Explanation of the main parts of the diagram 1 - Pin 2 - Template 3 - Dam 4 - Base play 1, 5 - Molding material Patent applicant Mitsubishi Heavy Industries, Ltd. Figure 3

Claims (1)

【特許請求の範囲】[Claims] 繊維とイj(脂からなる複合材料を圧縮成形するに際し
、圧縮力により前記複合材料中にビンを嵌入してボール
を同時に成形することを特徴とする複合材料のホール成
形方法。
1. A method for forming holes in a composite material, characterized in that when compression molding a composite material made of fibers and fat, a bottle is inserted into the composite material by compression force to mold a ball at the same time.
JP58118620A 1983-06-30 1983-06-30 Method of molding hole in composite material Pending JPS6011320A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP58118620A JPS6011320A (en) 1983-06-30 1983-06-30 Method of molding hole in composite material

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP58118620A JPS6011320A (en) 1983-06-30 1983-06-30 Method of molding hole in composite material

Publications (1)

Publication Number Publication Date
JPS6011320A true JPS6011320A (en) 1985-01-21

Family

ID=14741041

Family Applications (1)

Application Number Title Priority Date Filing Date
JP58118620A Pending JPS6011320A (en) 1983-06-30 1983-06-30 Method of molding hole in composite material

Country Status (1)

Country Link
JP (1) JPS6011320A (en)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4980217A (en) * 1988-07-29 1990-12-25 Grundfest Michael A Printed circuit board fabrication
US5268055A (en) * 1991-10-31 1993-12-07 Bales John L Method for making perforated composite laminates
US8057623B2 (en) 2006-07-14 2011-11-15 Airbus Operations Limited Composite manufacturing method
JP2012513913A (en) * 2008-12-30 2012-06-21 エムアールエイ・システムズ・インコーポレイテッド Process and apparatus for making composite structures
JP2012513914A (en) * 2008-12-30 2012-06-21 エムアールエイ・システムズ・インコーポレイテッド Process and apparatus for manufacturing composite structures
US20180290391A1 (en) * 2017-04-07 2018-10-11 General Electric Company Methods and Assemblies for Forming Features in Composite Components
JP2018200045A (en) * 2017-04-07 2018-12-20 ゼネラル・エレクトリック・カンパニイ Method and assembly for forming feature in composite material component
JP2019019818A (en) * 2017-04-07 2019-02-07 ゼネラル・エレクトリック・カンパニイ Method and assembly for forming feature in composite component

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5122028A (en) * 1974-08-19 1976-02-21 Hitachi Ltd
JPS5736619A (en) * 1980-08-14 1982-02-27 Matsushita Electric Works Ltd Perforation processing for synthetic resin molded product

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5122028A (en) * 1974-08-19 1976-02-21 Hitachi Ltd
JPS5736619A (en) * 1980-08-14 1982-02-27 Matsushita Electric Works Ltd Perforation processing for synthetic resin molded product

Cited By (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4980217A (en) * 1988-07-29 1990-12-25 Grundfest Michael A Printed circuit board fabrication
US5268055A (en) * 1991-10-31 1993-12-07 Bales John L Method for making perforated composite laminates
US8057623B2 (en) 2006-07-14 2011-11-15 Airbus Operations Limited Composite manufacturing method
US9764518B2 (en) 2006-07-14 2017-09-19 Airbus Operations Limited Composite manufacturing method
JP2012513913A (en) * 2008-12-30 2012-06-21 エムアールエイ・システムズ・インコーポレイテッド Process and apparatus for making composite structures
JP2012513914A (en) * 2008-12-30 2012-06-21 エムアールエイ・システムズ・インコーポレイテッド Process and apparatus for manufacturing composite structures
US20180290391A1 (en) * 2017-04-07 2018-10-11 General Electric Company Methods and Assemblies for Forming Features in Composite Components
CN108691580A (en) * 2017-04-07 2018-10-23 通用电气公司 It is used to form the method and sub-assembly of the feature in composite component
JP2018200045A (en) * 2017-04-07 2018-12-20 ゼネラル・エレクトリック・カンパニイ Method and assembly for forming feature in composite material component
JP2019006105A (en) * 2017-04-07 2019-01-17 ゼネラル・エレクトリック・カンパニイ Method and assembly for formation of fixture in composite material part
JP2019019818A (en) * 2017-04-07 2019-02-07 ゼネラル・エレクトリック・カンパニイ Method and assembly for forming feature in composite component
JP2020051427A (en) * 2017-04-07 2020-04-02 ゼネラル・エレクトリック・カンパニイ Methods and assemblies for forming features in composite components
US10632650B2 (en) 2017-04-07 2020-04-28 General Electric Company Methods and assemblies for forming features in composite components
US10737444B2 (en) 2017-04-07 2020-08-11 General Electric Company Methods and assemblies for forming features in composite components

Similar Documents

Publication Publication Date Title
CN1098152C (en) Dual purpose lay-up tool
KR100583036B1 (en) Hybrid lay-up tool
CN103286889A (en) Machinable composite mold
JP5111068B2 (en) Method for producing perforated fiber reinforced composite
US6620369B1 (en) Net molding of resin composite parts
US6811733B2 (en) Resin transfer molding multi-part/shim tooling (RTM-MPST)
US4335182A (en) Method of producing a molded composite foam body provided with a cover layer and the resultant product
JPS6011320A (en) Method of molding hole in composite material
US4509358A (en) Urethane dies
DE4300627C2 (en) Process for clamping a casting or forging
DE69911594T2 (en) METHOD FOR PRODUCING REINFORCED COMPOSITE STRUCTURES
JPH11512670A (en) A method for precision preforming of complex composite products
JPH05193025A (en) Manufacture of compound forming tool
JPH0357853B2 (en)
GB2039821A (en) Manufacture of Articles from Fibre-reinforced Plastics Material
EP0374186A1 (en) A composite body and a method for making the same.
US4737211A (en) Process for fabrication of graphite/epoxy tools
DE4300643A1 (en) Positioning and retention of deformation-sensitive workpiece
GB2254820A (en) Tooling for composite component manufacture
JP2573977B2 (en) Forming method of honeycomb core composite
JP2001315228A (en) Method for manufacturing honeycomb sandwich structure using composite material and molding device used therein
JP2730946B2 (en) Composite material molding method
CN219968899U (en) High-precision carbon fiber plate manufacturing tool
JP2685490B2 (en) Method for manufacturing composite mold
DE102013209179A1 (en) Method for the repair of components